User:DonaldLflr/sandbox


 * $$\begin{align}

t &= \gamma ( t' + v x'/c^2) \\ x &= \gamma ( x' + v t') \\ y &= y' \\ z &= z'. \end{align}$$


 * {| border="0" cellpadding="2"

!style="text-align: right"| $$T$$, !style="text-align: right"| $$R$$ !style="text-align: right"| $$M$$, !style="text-align: right"| $$\gamma$$ !style="text-align: right"| $$c_\text{p}$$, !style="text-align: right"| $$c_\text{v}$$, !style="text-align: right"| $$v_\text{e}$$, !style="text-align: right"| $$p_\text{e}$$, !style="text-align: right"| $$p$$,
 * style="text-align: left" | absolute temperature of gas at inlet (K)
 * style="text-align: left" | ≈ 8314.5J/kmol·K, universal gas law constant
 * style="text-align: left" | molecular mass or weight of gas (kg/kmol)
 * style="text-align: left" | $$= c_\text{p}/c_\text{v}$$, isentropic expansion factor
 * style="text-align: left" | specific heat capacity, under constant pressure, of gas
 * style="text-align: left" | specific heat capacity, under constant volume, of gas
 * style="text-align: left" | velocity of gas at nozzle exhaust (m/s)
 * style="text-align: left" | absolute pressure of gas at nozzle exhaust (Pa)
 * style="text-align: left" | absolute pressure of gas at inlet (Pa)
 * }